# Service difficulty reports: N796AX, cancelled Sep 29, 2021

A list on [N796AX, cancelled Sep 29, 2021](https://openairdocs.org/deregistered/N796AX-2021-09-29.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR ABXA200910300060](https://openairdocs.org/sdr/ABXA200910300060.md): Structure · cracked · Oct 28, 2009 · N796AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > NOSE WHEEL WELL VERTICAL CHORD AT LBL 25 AND STA 287 IS CRACKED IN RADIUS APP.687 INCH IN LENGTH. LOCATED 11.5 INCHES BELOW W/W CEILING PNL. REPAIRED VERTICAL CHORD AT LBL 25 AND STA 287 IAW B767 SRM 51-70-12.
- [SDR ABXA200910300058](https://openairdocs.org/sdr/ABXA200910300058.md): Jackscrew · corroded · Oct 28, 2009 · N796AX · Boeing 767281 · Stabilizer Actuator
  > AREA OF DISTORTION ON BALL SCREW THREAD AND SMALL SPOT OF CORROSION ON BOTTOM THREAD OF JACKSCREW. REMOVED AND REPLACED HORIZONTAL STAB JACKSCREW IAW B767 AMM 27-41-4.
- [SDR ABXA200910300057](https://openairdocs.org/sdr/ABXA200910300057.md): Fitting · cracked · Oct 28, 2009 · N796AX · Boeing 767281 · Fuselage Miscellaneous Structure
  > FORWARD LOWER CARGO DOOR CUTOUT CENTER HORIZONTAL ROLLER GUIDE FITTING CRACKED. CRACK LENGTH 4.5 INCH. ROLLER FITTING MISSING ALL 4 BOLTS (PUT TOGETHER WITH PIN). REMOVED AND REPLACED FITTING IAW B767-200 SRM 51-40-02.
- [SDR ABXA200910300056](https://openairdocs.org/sdr/ABXA200910300056.md): Cowling · cracked · Oct 28, 2009 · N796AX · Boeing 767281 · Engine Cowling System
  > NR 2 ENG O/B FAN COWL IS CRACKED ON EXTERIOR SURFACE AFT OF STATIC SENSE PORT. CRACK LENGTH 4 INCHES. REMOVED NR 2 ENG O/B COWL. REPAIRED ON WO 10074-0006. RE-INSTALLED NR 2 ENG O/B COWL REF AMM 71-11-04.
- [SDR ABXA080218](https://openairdocs.org/sdr/ABXA080218.md): Bolt · missing · Aug 9, 2008 · N796AX · Boeing 767281 · Fuselage, Landing Gear Attach Fittings
  > LT MAIN LANDING GEAR TRUNNION DOOR FITTING ON TOP OF STRUT MISSING AFT BOLT AND ATTACHING HARDWARE. INSTALLED CORRECT HARDWARE PER IPC 32-12-01-5, SHEET 2 AND AMM 32-12-06. (BOLTS 2 EA-BACB30LJ6U15). (S)
- [SDR ABXA080110](https://openairdocs.org/sdr/ABXA080110.md): Light · inoperative · Mar 19, 2008 · N796AX · Boeing 767281 · Emergency Lighting
  > MAINTENANCE AT ILN FOUND MAIN ENTRY DOOR EMERGENCY ESCAPE LIGHT LENS CRACKED AND LIGHT INOP. REMOVED AND REPLACED MAIN ENTRY DOOR EMERGENCY ESCAPE LIGHT ASSEMBLY IAW B767 AMM 33-51-06-2.
- [SDR ABXA080062](https://openairdocs.org/sdr/ABXA080062.md): Door Frame · corroded · Jan 29, 2008 · N796AX · Boeing 767281 · Cargo/Baggage Doors
  > FORWARD LOWER CARGO DOOR FRAME UNDER VENT DOORS CORRODED IN SEVERAL PLACES. REMOVED AND REPLACED FORWARD LOWER CARGO DOOR FRAME IAW B767 SRM.
- [SDR ABXA080061](https://openairdocs.org/sdr/ABXA080061.md): Beam · corroded · Jan 28, 2008 · N796AX · Boeing 767281 · Cargo/Baggage Doors
  > I-BEAM DIRECTLY BELOW DEPRESSURIZATION VENTS ON AFT LOWER CARGO DOOR HEAVILY CORRODED. REMOVED AND REPLACED BEAM IAW B767 SRM 51-40-2.
- [SDR ABXA060228](https://openairdocs.org/sdr/ABXA060228.md): Strap · corroded · Jul 6, 2006 · N796AX · Boeing 767281 · Wing, Rib/Bulkhead
  > UPPER SPAR CAP STRAP AT RT WING STA 792 HAD INTERGRANULAR CORROSION. REPAIRED AREA IAW REA B657-54341.
- [SDR ABXA060227](https://openairdocs.org/sdr/ABXA060227.md): Shear Tie · corroded · Jul 6, 2006 · N796AX · Boeing 767281 · Fuselage Internal Mounting Structure
  > FRAME CORRODED AT STA 1219 BETWEEN S38-47R. REMOVED AND REPLACED SHEAR TIE IAW B767 SRM 51-40-02.
- [SDR ABXA040050](https://openairdocs.org/sdr/ABXA040050.md): Module · leaking · Jan 29, 2004 · N796AX · Boeing 767281 · Hydraulic Reservoir, Main
  > CENTER HYDRAULIC QUANTITY DECREASED TO.13, SYSTEM DEPRESSURIZED AND LEAK CONTINUED. ON APPROACH, COMPLETE LOSS OF CENTER HYDRAULICS. FOUND FLAP/SLAT SHUTOFF VALVE MODULE ASSEMBLY LEAKING AT FILTER HOUSING. REPLACED FLAP/SLAT SHUTOFF VALVE MODULE ASSEMBLY I
- [SDR ABXA030345](https://openairdocs.org/sdr/ABXA030345.md): Duct · out of adjust · Sep 3, 2003 · N796AX · Boeing 767281 · Air Distribution System
  > MAINTENANCE COULD NOT OPEN R-2 WINDOW. FOUND WINDOW BINDING ON LOWER AC DUCT. ADJUSTED AND SECURED AC DUCT. WINDOW OPENED NORMALLY.
- [SDR ABXA030194](https://openairdocs.org/sdr/ABXA030194.md): Panel · gouged · Jun 10, 2003 · N796AX · Boeing 767281 · Nacelle/Pylon, Plate/Skin
  > DURING INSPECTION, TWO GOUGES WERE FOUND ON NR 1 ENGINE STRUT RIGHT SKIN PANEL NEAR AN ACCESS DOOR CUTOUT. MAXIMUM DEPTH OF BLEND OUT REQUIRED TO COMPLETELY REMOVE DAMAGE WAS 0.035 INCH. REPAIRED AREA IAW REA B654-46243MR.
- [SDR ABXA030193](https://openairdocs.org/sdr/ABXA030193.md): Door Frame · corroded · Jun 10, 2003 · N796AX · Boeing 767281 · Cargo/Baggage Doors
  > AFT CARGO DOOR BEAM NR 5, CORROSION WAS FOUND ON THE INNER CHORD P/N 140T2605-3 UNDERNEATH PUMP. AFTER CORROSION REMOVED MINIMUM REMAINING THICKNESS WAS 0.082, WHILE ORIGINAL THICKNESS WAS 0.125 INCH.
- [SDR ABXA030192](https://openairdocs.org/sdr/ABXA030192.md): Strut · gouged · Jun 10, 2003 · N796AX · Boeing 767281 · Nacelle/Pylon, Main Frame
  > DURING INSPECTION, TWO GOUGES WERE FOUND ON NR 2 ENGINE STRUT RIGHT SKIN PANEL NEAR ACCESS DOOR CUT OUT. MAXIMUM DEPTH OF BLENDED OUT REQUIRED TO COMPLETELY REMOVE DAMAGE, 0.025 INCH. REPAIRED AREA IAW REA.
- [SDR ABXA030198](https://openairdocs.org/sdr/ABXA030198.md): Frame · corroded · Jun 10, 2003 · N796AX · Boeing 767281 · Fuselage Main, Frame
  > RIGHT STA. 883.5 FRAME SEGMENT P/N 145T1003-2 FAIL SAFE FRAME AT STR. 18 RIGHT WAS FOUND CORRODED. THE ORIGINAL THICKNESS OF FRAME WAS 0.200 INCH AFTER BLENDED OUT CORROSION THE REMAINING THICKNESS WAS 0.170 INCH. REPAIRED AREA IAW REA B653-46282, REV. 'A'.
- [SDR ABXA030197](https://openairdocs.org/sdr/ABXA030197.md): Skin · gouged · Jun 10, 2003 · N796AX · Boeing 767281 · Cargo/Baggage Doors
  > CARGO DOOR GOUGE WAS FOUND IN THE PART AT BULK CARGO DOOR INNER SKIN, STA. 1439, WL 131, P/N 146T6334-1, GOUGE ON INNER SKIN. REPAIRED AREA IAW REA MR.
- [SDR ABXA030196](https://openairdocs.org/sdr/ABXA030196.md): Stringer · corroded · Jun 10, 2003 · N796AX · Boeing 767281 · Horizontal Stabilizer, Spar/Rib
  > RIGHT HORIZONTAL STAB. LOWER STRINGER NO. 10 LOWER HORZ. FLANGE RBL 56, P/N 181T4110-4, FOUND CORROSION DURING INSPECTION ON STRINGER P/N 181T4110-4 COMMON TO SKIN PANEL REMAIN THICKNESS MATERIAL OF 0.135 INCH ORIGINAL THICKNESS WAS 0.165 INCH. THE TOTAL BLE
- [SDR ABXA030195](https://openairdocs.org/sdr/ABXA030195.md): Fitting · elongated · Jun 10, 2003 · N796AX · Boeing 767281 · Nacelle/Pylon Miscellaneous Structure
  > DURING INSPECTION, ON LEFT STRUT FORWARD UPPER SPAR FITTING, FOUND FOUR BOLT HOLES SHOULD BE.4375 INCH ARE ALREADY OVERSIZED TO 0.515 INCH AND BACB 30 MT8X ARE INSTALLED. SB GIVES A MAXIMUM OVERSIZE OF 4692 INCH FOR THOSE HOLES. REWORKED AREA IAW REA B654-462
- [SDR ABXA030191](https://openairdocs.org/sdr/ABXA030191.md): Frame · damaged · Jun 10, 2003 · N796AX · Boeing 767281 · Nacelle/Pylon, Frame/Spar/Rib
  > NR 2 ENGINE RIGHT CORE COWL FRAME NAS STA. 304.60 AND NAC WL 73, DAMAGE WAS FOUND ON FRAME P/N 314T1210-333. REPAIRED AREA IAW REA B671-46254MR.
- [SDR ABXA030285](https://openairdocs.org/sdr/ABXA030285.md): Support Fitting · damaged · Jun 5, 2003 · N796AX · Boeing 767281 · Wing Miscellaneous Structure
  > RIGHT WING TRAILING EDGE 113T1647-6 PANEL SUPPORT FITTING ASSEMBLY DAMAGED DOUBLE HOLE AND BLENDED AREA STA 1051 RIGHT BUTTLINE 97.4. REPAIRED AREA IAW REA B657-46309MR.
- [SDR ABXA030184](https://openairdocs.org/sdr/ABXA030184.md): Wire · damaged · Mar 16, 2003 · N796AX · Boeing 767281 · APU System Wiring
  > APU GENERATOR FEEDER WIRE DAMAGE, CAUSED SHORT CIRCUIT TO GROUND, RESULTING ARCHING TO WIRE AND CLAMP AT STA 1788 RIGHT. REPLACED THE FEEDER WIRE FROM THE NEARBY SPLICE TO APU SHROUD CONNECTOR D 4016J, AND CLAMP. OPS CHECKED GOOD IAW B767 MM.
- [SDR ABXA030014](https://openairdocs.org/sdr/ABXA030014.md): Floorbeam · corroded · Nov 20, 2002 · N796AX · Boeing 767281 · Fuselage Main, Floor Beam
  > CABIN RIGHT SIDE STA 287 FLOORBEAM, RBL 73, FOUND CORROSION ON UPPER FLANGE OF FLOORBEAM, WL 199.5. PERFORMED FLOORBEAM UPPER CHORD REPAIR IAW SRM 53-00-51, FIGURE 201, REF SRM 53-10-51 AND DWG NR 141T5111. INSTALLED IAW SRM 51-40-02.

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N796AX' AND deregistration_id = 'N796AX-2021-09-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N796AX-2021-09-29/reports

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